N968AS

Part: VANE — CHAFED (TE FLAP) · airframe 51,967 hrs · 25,742 cycles

RIGHT WING O/B FLAP I/B VANE REPAIR DOUBLER IS CHAFED AT I/B CORNER. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AND FABRICATED REPAIR DOUBLER, LOADED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PG 11 PAR 6 23 59.

Part: FLOOR PANEL — BROKEN (BS 256) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL STA 200 TO STA 256 LBL16 TO RBL 22 PULLED OUT AND DAMAGED BROKEN INSERTS. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 53 05 PGS 251, 257 AND DAC DRAWING S4932106.

Part: SEAT TRACK — CORRODED (BS 1130-1211) · corrosion level 1 · airframe 51,967 hrs · 25,742 cycles

CABIN SEAT TRACK CORRODED STA 1211 TO 1130 LBL 44. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SEAT TRACK AND SPLICES IAW MD 80 SRM 53-05 FIG 4B 1 AND FIG 4 F.

Part: VANE — DENTED (TE FLAP) · airframe 51,967 hrs · 25,742 cycles

RIGHT WING I/B FLAP I/B VANE LWR SURFACE HAS GRAVEL DAMAGE (DENTED). PREPARED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER BONDED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PGS 23, 43, 46, 59, 63 AND 64.

Part: FLOOR PANEL — CORRODED (BS 196-256) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL CORRODED AND BROKEN INSERTS STA 196 TO STA 256 LBL 16 TO LBL 22. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD 80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.

Part: INTERCOSTAL — CORRODED (BS 228-237) · corrosion level 1 · airframe 51,967 hrs · 25,742 cycles

INTERCOSTAL UPPER FLANGS EXFOILATED STA 228 AT LBL 34. REMOVED DAMAGED INTERCOSTAL, LOCATED DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL AND REPAIR PARTS FOR WIRE FEED THRU IAW MD80 SRM 51-30-5 PG 1, 53-01 FIG 2 PG 13.

Part: FLOOR PANEL — CORRODED (BS 160-195) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL STA 160 TO STA 195 LBL 8 TO LBL 44 BROKEN AND CORRODED INSERTS. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S 4932106.

Part: FLOOR PANEL — PUNCTURED (BS 1117-1174) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL STA 1117 TO STA 1174 BL 0 TO RBL 22. PUNCTURED, FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW MD 80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.

Part: FLOOR PANEL — PUNCTURED (BS 1097-1117) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL STA 1097 TO STA 1117 LBL 22 TO RBL 22 PUNCTURED. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.

Part: SEAT TRACK — CORRODED (BS 1042-1231) · corrosion level 1 · airframe 51,967 hrs · 25,742 cycles

CABIN SEAT TRACK CORRODED TOP AND BOTTOM STA 1042 TO STA 1231 AT LBL 22. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SEAT TRACK AND SPLICE DOUBLERS IAW MD80 SRM 51-10-4 PGS 1 AND 2, 53-05 FIG 4F SHTS 1 & 2.

Part: FLOOR PANEL — PUNCTURED (BS 1174-1250) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL STA 1174 TO STA 1250 LBL 22 TO RBL 22. PUNCTURED, FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.

Part: FLOOR PANEL — CORRODED (BS 180) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOORBOARD STA 160 TO STA 180 RBL 8 TO RBL 44 CORRODED. INSERTS FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106.

Part: FLOOR PANEL — PUNCTURED (BS 1117-1174) · airframe 51,967 hrs · 25,742 cycles

CABIN FLOOR PANEL STA 1117 TO STA 1174 BL 0 TO LBL 22 PUNCTURED. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DWG S4932106.

Part: VANE — GOUGED (TE FLAP) · airframe 51,967 hrs · 25,742 cycles

LEFT WING O/B FLAP I/B VANE GOUGED ON L/E AREA MARKED. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AREA, FABRICATED REPAIR DOUBLER BONDED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PG 11 23 PAR 10C PG 32 AND PAR 18B PG 91.

Part: VANE — DELAMINATED (FLAP) · airframe 51,967 hrs · 25,742 cycles

LEFT INBOARD FLAP OUTBOARD FLAP VANE DELAMINATED ON UPPER SURFACE 53 INCHES FROM OUTBOARD END. PREPARED DAMAGED AREA, FABRICATED FILLER AND DOUBLER REPAIR PARTS, LOADED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PAT 18B PGS 91 95.

Part: SKIN — DENTED (L1 DOOR) · airframe 51,967 hrs · 25,742 cycles

LEFT EXT FUSELAGE SKIN AFT OF L1 DOOR DENT OUT OF LIMITS STA 213 ABOVE LONG 166 DIA = .800 DEPTH = .034 RATIO OF 23.52 RECON TOURED DENT YAW MD80 SUM 53 04 FIG 38. HEFT INSPECTED, NO CRACKS NOTED YAW MD80 SUM 53 04 FIG 38 AND NUDISM PT 6.06 10 00 001. FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLERS REPAIR YAW MD80 SUM 53 04 VIEW E.

Part: FLOOR SUPPORT — DAMAGED (BS 160-200) · corrosion level 2 · airframe 51,967 hrs · 25,742 cycles

REMOVED DAMAGED CABIN FLOOR TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT TRACK IAW MD80 SRM 51-10-4 PG 1.

Part: CUSP WEB — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 51,967 hrs · 25,742 cycles

RIGHT CUSP WEB CORRODED STA 1212 TO STR 1231. REMOVED, CUT OUT DAMAGED AREA OF CUSP WEB, FABRICATED DOUBLER, LOCATED DRILLED AND INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-05 PG 563 FIG 96.

Part: LONGERON — CRACKED (BS 264-323) · airframe 50,838 hrs · 25,196 cycles

LONGERON CRACKED. CUT OUT DAMAGED AREA. INSTALLED REPLACEMENT SECTION WITH LONGERON SPLICES PER SRM 51-10-4 AND SRM 53-02.

Part: SKIN — DENTED (BS 279-303) · airframe 50,838 hrs · 25,196 cycles

FUSELAGE DENTED BEYOND SRM 53-4 LIMITS. CUT OUT DAMAGED AREA OF SKIN. INSTALLED FILLERS FINGER DOUBLERS AND REPAIR DOUBLER PER SRM 53-4 AND SRM 51-10-3.

Part: SKIN — SCRATCHED (FUSELAGE)

LARGE SCRATCHES ON LEFT FUSELAGE. REMOVED DAMAGED AREA. INSTALLED TWO EXTERNAL REPAIR DOUBLERS PER SRM 53-4.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 49,904 hrs · 24,745 cycles

L1 DOOR SKIN AT UPPER CORNER PEELED BACK. REMOVED DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 52 05. PERFORMED CLASS III REPAIR PER SRM 53 04.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,156 hrs · 24,387 cycles

FUSELAGE CORRODED AFT OF LAV SERVICE PANEL. REPAIRED PER EA 5330 02145.

Part: SKIN — DENTED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

LEFTHAND INBOARD FLAP OUTBOARD VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-2.

Part: SKIN — GOUGED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

LEFT INBOARD FLAP OUTBOARD VANE L/E GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — DENTED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

RIGHTHAND OUTBOARD FLAP VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — GOUGED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

LEFTHAND INBOARD FLAP OUTBOARD VANE IS GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — DENTED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

RIGHTHAND OUTBOARD FLAP INBOARD VANE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — DENTED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

LEFTHAND INBOARD FLAP OUTBOARD VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.

Part: SKIN — DENTED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

RIGHTHAND OUTBOARD FLAP INBOARD VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — GOUGED (FLAP VANE) · airframe 48,795 hrs · 24,209 cycles

LEFTHAND OUTBOARD FLAP VANE L/E GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: INTERCOSTAL — CORRODED (BS 700-720) · corrosion level 2 · airframe 48,795 hrs · 24,209 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 53-01 51-30-05 AND 51-10-3.

Part: SHEAR TIE — CORRODED (BS 636 S29-30R) · corrosion level 2 · airframe 48,795 hrs · 24,209 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 30 5.

Part: SUPPORT — CRACKED (BS 1287 S27-28L) · airframe 48,795 hrs · 24,209 cycles

FOUND FRAME SUPPORT CRACKED. REPLACED SUPPORT PER SRM 51 30 5.

Part: TAB — CRACKED (ELEVATOR) · airframe 48,795 hrs · 24,209 cycles

RIGHT HAND ELEVATOR CONTROL TAB EDGE CRACKED. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 48,795 hrs · 24,209 cycles

FOUND GUSSET CORRODED. REPLACED GUSSET PER DWG 5936071 AND SRM 51 30 5.

Part: FLOOR PANEL — DEBONDED · airframe 48,795 hrs · 24,209 cycles

FOUND CABIN FLOORBOARD PANEL EDGE DISBONDED. REPLACED PANEL PER SRM 53 05 AND DWG 9936651.

Part: SPLICE — CORRODED (BS 417 S27R) · airframe 48,795 hrs · 24,209 cycles

FOUND FORWARD CARGO DOOR JAMB SPLACE CORRODED. REPLACED SPLICE PER SRM 51 10 3 AND 51 30 5.

Part: TAB — DENTED (LT ELEVATOR) · airframe 48,795 hrs · 24,209 cycles

FOUND LEFT ELEVATOR CONTROL TAB LOWER SURFACE DENTED. FILLED DENT PER SRM 55 04.

Part: SKIN — DENTED (BS 676) · airframe 48,795 hrs · 24,209 cycles

FOUND MID CARGO BAY DOOR DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 52 05.

Part: TAB — DENTED (RT ELEVATOR) · airframe 48,795 hrs · 24,209 cycles

RIGHT HAND ELEVATOR GEAR TAB UPPER SURFACE DENTED. BONDED DENTED AREA PER SRM 51-70-2.

Part: SKIN — GOUGED (BS 229-272) · airframe 48,795 hrs · 24,209 cycles

FOUND FUSELAGE SKIN REPAIR DOUBLER GOUGED. REPLACED DOUBLER PER SRM 53 04.

Part: TAB — DENTED (LT ELEVATOR) · airframe 48,795 hrs · 24,209 cycles

LEFT ELEVATOR CONTROL TAB UPPER SURFACE DENTED. FILLED DENT PER SRM 55 04.

Part: SKIN — CORRODED (AUX FUEL TANK) · corrosion level 2 · airframe 48,795 hrs · 24,209 cycles

AUX FUEL TANK ACCESS PANEL MOUNTING FLANGE CORRODED. REPLACED DOUBLER PER DWG 5936434 AND SRM 51 30 5.

Part: SPLICE — CORRODED (BS 1215-1227) · corrosion level 2 · airframe 48,795 hrs · 24,209 cycles

FOUND LONGERON SPLICE CORRODED. REPLACED SPLICE PER SRM 53 02 AND 51 30 5.

Part: SKIN — GOUGED (LT WING TE FLAP)

OKC - DURING HV CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD LEADING EDGE IS GOUGED. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 1067)

OKC - FOUND HV-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 1102-1105. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FLOOR PANEL 6-C IS MISSING SEVERAL INSERTS. REMOVED AND REPLACED FLOORBOARD. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 1057-1060. REMOVED DAMAGED SECTION. INSTALLED A REPAIR DOUBLER. (M)

Part: FRAME — CORRODED (FS)

OKC - DURING HV-CHECK, FRAME AT STATION 1231 LONGERON 30 AND 29R IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER, WEB, AND ANGLES. (M)

Part: WEB — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FLOOR WEB STATION 190 RBL 30 HAS A CRACK ABOVE THE RACK ON THE RIGHT SIDE OF E/E BAY. REMOVED DAMAGE AND REPLACED WITH DOUBLER. (M)

Part: SKIN — CHAFED (CARGO DOOR)

OKC - DURING HV CHECK, FOUND MID CARGO DOOR, AFT INBOARD SKIN NEAR DOOR HANDLE IS CHAFFED. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M)

Part: CHANNEL — CUT (FS)

OKC - DURING HV-CHECK, FOUND FLOOR PANEL 4-E HAT SECTION HAS .25 INCH LONG CUTS AT THE END OF THE HAT SECTION. REMOVED DAMAGED SECTION OF HAT CHANNEL. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND HV CHECK, FOUND DENT IN FUSELAGE NEAR FORWARD LAV SERVICE DOOR, LENGTH 1.640625 BY 1.390625 WIDE BY .171875 DEEP. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND LEFT FLOOR CUSP WEB CORRODED AT STATION 465-389. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, LEFT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 389-503. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

OKC - FOUND DURING HV CHECK, LEFT OUTBOARD CABIN FLOOR PANEL AT STATION 465-541 HAS CRACKED HAT CHANNEL. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV-CHECK, FOUND LEFT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DELAMINATED (WING)

OKC - DURING HV-CHECK, FOUND LEFT ANTI-FLOAT TAB HAS A COMPOSITE REPAIR ON TRAILING EDGE, LOWER SURFACE IS DELAMINATING. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER. (M)

Part: FLOORBOARD — CRACKED (FS 693-617)

OKC - DURING HV CHECK, FOUND FLOOR PANEL E-8 IS MISSING SPACER IN SUPPORT. REMOVED DAMAGED SECTION OF HAT CHANNEL DUE CRACK. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

OKC - DURING HV-CHECK, FOUND E3 FLOOR PANEL HAS A CRACKED SUPPORT. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CHANNEL — BROKEN (FUSELAGE)

OKC - DURING HV-CHECK, RIGHT FLOORBOARD 4 E HAT CHANNEL HAS BROKEN FASTENER HOLE. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV-CHECK, RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, E12 FLOOR PANEL HAS A CRACKED STIFFENER ON THE LOWER SIDE. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - FOUND HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 256-275. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 1174-1250)

OKC - DURING C-CHECK, FOUND CABIN FLOOR CUSP WEB IS CORRODED. REMOVED DAMAGE AND INSTALLED DOUBLER. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FUSELAGE SKIN HAS DENT AT STATION 211 BELOW 14R. RECONDITIONED SKIN AND INSTALLED DOUBLER. (M)

Part: RELIEF VALVE — FAILED (RT ENGINE)

CLIMB, OIL PRESSURE AND QUANTITY INDICATIONS DROPPED BELOW ACCEPTABLE LEVELS. ENGINE WAS SHUTDOWN IN FLIGHT, AND ATB TO LAX WAS EXCUTED. REMOVED AND REPLACED ENGINE DUE INDICATION OF INTERNAL FAILURE. REPLACED OIL PRESSURE RELIEF VALVE. OP AND LEAK CHECKED OK. NO INTERNAL FAILURE FOUND. (K)

Part: LANYARD — DISCONNECTED (L2 DOOR SLIDE)

SEA - DURING PREFLIGHT CHECK, FOUND AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: NOSE COWL — CRACKED (LT ENGINE)

OKC - DURING HV6-CHECK, LEFT ENGINE NOSE COWL IS CRACKED AT AFT FLANGE 7 O'CLOCK POSITION. REMOVED DAMAGED SECTION. REPAIRED WITH DOUBLER AND FILLER PER EA 7110-01221. (M)

Part: SLAT TRACK — GOUGED (L/E SLAT)

OKC - DURING HV6 CHECK, FOUND NR 2 SLAT LEFT NR 8 TRACK HORN IS GOUGED ALONG LOWER EDGE. REMOVED DAMAGED SECTION AND PERFORMED HFEC REPAIR PER EA 5740-01380. (M)

Part: TUBE — CHAFED (L/E SLAT)

OKC - DURING HV6 CHECK, NR 5 SLAT LEFT BLOW TUBE CONNECTION END WORN ALONG EDGE. WELD-REPAIRED CHAFED AREA AND RECONTOURED TO ORIGINAL SHAPE PER EA 3010-01075. (M)

Part: SKIN — CORRODED (NR 1 SLAT)

OKC - DURING HV6- CHECK - FOUND NR 1 SLAT FORWARD INBOARD PIN MATING SURFACE AND CASTING HOLE IS CORRODED. REAMED HOLE AND INSTALLED BUSHING EPR EA 5740-01382. (M)

Part: ACCESS PANEL — CORRODED (LT WING)

OKC - DURING HV6 CHECK, FOUND LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M)

Part: WINDOW FRAME — CHAFED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND FRAME AROUND AFT FRAME OF CAPTAINS SLIDING WINDOW CHAFED. BLENDED, TREATED, AND PRIMED CHAFED AREA PER EA 5310-02315. (M)

Part: VANE — WORN (T/E FLAP)

OKC - DURING HV6 CHECK, FOUND RIGHT WING OUTBOARD FLAP VANE INBOARD AFT EDGE IS WORN. BLENDED OUTBOARD FLAP TRAILING EDGE. FOUND TO BE IN LIMITS IAW ASA EA 5750-01923, AND AAR EA 10283. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS CORRODED OUTBOARD OF OUTBOARD TRACK AT FS 256-313. REPLACED PANEL PER SRM 53-05. (M)

Part: DOOR FRAME — CRACKED (CARGO DOOR)

OKC - DURING HV6 CHECK, FOUND AFT CARGO DOOR CRACKED AT OUTBOARD FRAME ON TRAILING EDGE OF DOOR JUST ABOVE AND OUTBOARD OF DOOR LATCH TORQUE TUBE. STOP DRILLED CRACK, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 52-03 AND NDTM PT6. (M)

Part: INTERCOSTAL — CORRODED (FS)

OKC - DURING HV6-CHECK, FOUND CORROSION ON NUT PLATES AND SEAT TRACK MID PIT STATION 769 TO 788 STRINGER 28R. REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW MD80 SRM 51-30-2. (M)

Part: ACCESS PANEL — CORRODED (LT WING)

OKC - DURING HV6-CHECK, LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND RIGHT INTERCOSTAL IS CORRODED AT FS 1309-1322. REPLACED INTERCOSTAL PER SRM 51-30-2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND AFT PIT STATION 1212 LONGERON 26L HAS CORROSION ON TOP OF SPLICE PLATE. REMOVED DAMAGED PLATE, FABRICATED AND INSTALLED REPLACEMENT PLATE IAW MD80 SRM 51-10-4. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND FUSELAGE SKIN DENTED AT FS 212-272. REPLACED EXISTING REPAIR DOUBLER AND FILLER PER SRM 50-04. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED AND BENT INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53-05. (M)

Part: HINGE — WORN (CARGO DOOR)

OKC - DURING HV6 CHECK, FOUND MID CARGO BAY DOOR HINGE BOLT HOLES ARE WORN FORWARD AND AFT. REPLACED DOOR HINGES PER OHM 52-30-1. (M)

Part: ACCESS PANEL — CORRODED (LT WING)

OKC - DURING HV6 CHECK, - FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1361 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M)

Part: SKIN — DENTED (T/E FLAP)

OKC - DURING HV6 CHECK, FOUND STRIP, ANTI-ABRASION COATING AT OUTBOARD LOWER END OF LEFT INBOARD FLAP WEDGE AND EVALUATE 3 DENTS. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR SKIN IAW MD80 SRM 51-70-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND PIT CORROSION ON TOP AND BOTTOM OF WEB BETWEEN STATION 1211 AND 1212 LONGERON 30 TO 28R. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-10-4. (M)

Part: RIB — CRACKED (NR 5 SLAT)

OKC - DURING HV6 CHECK, FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP RIB IS CRACKED AT RIVET HOLE. REPLACED DAMAGED END CAP RIB PER SRM 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND LEFT INTERCOSTAL IS CORRODED ON FLANGE AT FS 788. REPLACED INTERCOSTAL PER SRM 51-30-2. (M)

Part: SKIN — WORN (RUDDER)

OKC - DURING HV6 CHECK, FOUND RUDDER LOWER HINGE SKIN HAS WORN ASTRO STRIKE. REPLACED ASTRO STRIKE PER SRM 51-70-1A. (M)

Part: CUSP WEB — CRACKED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND FLOOR WEB CRACKED, FROM STATION 1287 TO 1309 AT 18R. REMOVED DAMAGED CUSP WEB, ORDERED AND INSTALLED NEW CUSP WEB IAW MD80 SRM 53-05 FIG 97. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND FORWARD CARGO COMPARTMENT STATION 247 CORROSION ON LONGERON 30. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE IAW MD80 SRM 53-02. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND SKIN DENTED/GOUGED AT FS 351. INSTALLED FILLER AND DOUBLER PER SRM 53-04. (M)

Part: ACCESS PANEL — CORRODED (LT WING)

OKC - DURING HV6-CHECK, FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1367 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND MID CARGO BAY DOOR JAMB FRAME INTERCOSTAL IS CORRODED ON FRAME SHEAR TIE AT FS 674. REPLACED INTERCOSTAL PER SRM 51-30-7. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CUSP WEB IS CORRODED AT FS 256. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-70-4. (M)

Part: INSERT — CORRODED (FLOOR PANEL)

OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED DAMAGED PANEL PER SRM 53-05. (M)

Part: STRAP — CORRODED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND MID PIT LOWER PAN, STRAP HAS CORROSION. REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED REPLACEMENT STRAP IAW MD80 SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND AFT PIT WEB AT DOOR CUTOUT BETWEEN STATION 1155 AND 1212 HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-10-4. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND AFT CARGO PIT CORROSION ON AFT AND FRONT SIDE OF FORMER AT STATION 1211 BETWEEN LONGERON 30 AND 22R. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW MD80 SRM 51-30-3. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE SEAL MISSING FS 1009-1041. RESEALED PER DPS 1.901 AND DWG 9936584. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND E/E COMPARTMENT FRAME CORRODED AT FS 200. REMOVED DAMAGED SECTION. INSTALLED SHIM, PLATE, AND ANGLE PER SRM 53-03. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND SEAT TRACK IS CORRODED AT FS 236-266. REPLACED DAMAGED SECTION PER SRM 51-30-1 AND 51-30-5. (M)

Part: WEB — CRACKED (L1 DOOR)

OKC - DURING HV6 CHECK, FOUND FORWARD PAX L1 DOOR TORQUE BOX WEB IS CRACKED. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND SHIM PER SRM 53-01. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL CORNER IS DELAMINATED AT FS 160-180. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE DELAMINATED AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS MISSING EDGE SEAL AT FS 886-905. RESEALED PANEL PER DPS 1.901 AND DWG 9936584. (M)

Part: SKIN — CRACKED (L1 DOOR)

OKC - DURING HV6-CHECK, FOUND FORWARD PAX L1 DOOR INNER SKIN IS CRACKED AT LOWER FORWARD CORNER. REMOVED PRIOR REPAIR AND INSTALLED REPLACEMENT DOUBLER PER SRM 52-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND SEAT TRACK IS CORRODED AT FS 236-313. REPLACED DAMAGED SECTION PER SRM 51-30-1 AND 51-30-5. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE SEAL MISSING FS 1007-1079. RESEALED PER DPS 1.901 AND DWG 9936584. (M)

Part: VANE — CHAFED (T/E FLAP)

OKC - DURING HVC CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD CAM AND VANE LEADING EDGE ARE CHAFED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2 AND 57-03. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE SEALANT MISSING AT FS 864-886. RESEALED EFFECTED AREAS. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS BROKEN INSERTS AND MISSING MATERIAL AT FS 465-541. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRUSHED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL CORNER IS CRUSHED AT FS 905-977. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS TORN EDGE AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M)

Part: INSERT — CORRODED (FLOOR PANEL)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 180-200. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL SIDE SUPPORT IS CRACKED AND DEFORMED AT FS 826-886. REPLACED SUPPORT PER SRM 51-10-4. (M)

Part: INSERT — MISSING (FLOOR PANEL)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS NUMEROUS MISSING, BROKEN AND CORRODED INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE SEALANT MISSING AT FS 826-864. RESEALED EFFECTED AREAS. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: INTERCOSTAL — GOUGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND AFT CARGO BAY DOOR BEAM INTERCOSTAL IS CORRODED AT FS 1193. REPLACED INTERCOSTAL PER SRM 51-10-4. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR INTERCOSTAL CRACKED AND BENT AT FS 1045. REPLACED INTERCOSTAL PER SRM 51-30-2. (M)

Part: FLOOR PANEL — GOUGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS GOUGED ALONG EDGE AT FS 905-977. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND AFT CARGO BAY DOOR BEAM INTERCOSTAL IS CORRODED AT FS 1165. REPLACED INTERCOSTAL PER SRM 51-10-4. (M)

Part: FLOOR PANEL — GOUGED (FUSELAGE)

OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AT EDGE AT FS 808-826. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

OKC - DURING HV-6 CHECK, FOUND AFT EXIT TAIL EMERGENCY ESCAPE SLIDE FAILED TO DEPLOY DURING OPERATIONAL CHECK. LANYARD PULLED LOOSE FROM SLIDE PACK COVER, AND COVER REMAINED IN POSITION. S/D - INVESTIGATION SUGGESTS THAT THE PROBABLE CAUSE OF FAILURE WAS A WORN VELCRO ATTACHMENT AT THE SLIDE COVER END OF THE RELEASE LANYARD. THIS ATTACHMENT, IN CONJUNCTION WITH A METAL SNAP, IS WHAT FASTENES THE LANYARD TO THE COVER. IT WOULD APPEAR THAT NEITHER, ALONE, IS SUFFICIENT UNDER TENSION TO KEEP THE LANYARD FASTENED TO THE COVER. LUBRICATION FLUIDS FROM THE EMPENNAGE TEND TO DROP ON THE SLIDE COVER, AND THIS MAY, OVERTIME, BE WHAT DAMAGED THE VELCRO. THE LANYARD WAS REPLACED. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (LIGHT MODULE)

SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 1 IN FIRST CLASS CABIN. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. REPLACED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SAN PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED AT ROW 3. RECONNECTED WIRING AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTORS AND REPLACED A COUPLE OF DAMAGED WIRE SEGMENTS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE IN 1ST CLASS CABIN. REPAIRED, RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

PDX - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN 1ST CLASS. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - DURING LINE CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, HORIZONTAL FLANGE UNDER AFT CARGO BAY DOOR BEAM DOUBLER IS CORRODED. REPLACED PREVIOUS DOUBLER AND SPACER PER EA 5310-02130. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, AFT CARGO BAY LEFT TIEDOWN TRACK IS CORRODED FROM FS 1212 TO 1338 AT LONGERON 27L. REPLACED TIEDOWN TRACK PER SRM 51-10-4 AND 51-30-0. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, AFT CARGO BAY LEFT TIEDOWN TRACK IS CORRODED FROM FS 1212 TO 1338. REPLACED TIEDOWN TRACK PER SRM 51-10-4 AND 51-30-0. (M)

Part: FRAME — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, AFT SIDE OF CIRCUMFERENTIAL FRAME IS CORRODED AT FS 588 BETWEEN LONGERON 28R AND 28L. REPAIRED WITH DOUBLER PER SRM 53-01, 53-03, 51-10-3, AND 51-10-3B. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OAK - FOUND ON C-CHECK, SPLICE CORRODED AT FS 1117-1136 ON LONGERON 30. REPLACED SPLICE PER SRM 53-01, 53-02, 51-10-3, 51-10-3B, AND 51-30-1. (M)

Part: FRAME — CORRODED (FUSELAGE)

CIRCUMFERENTIAL FRAME IS CORRODED AT FUS STA 588 BETWEEN LONGERON 28R AND 28L IN MID CARGO BAY. REPAIRED WITH DOUBLER IAW SRM.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

SEA - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

SEA - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M)

Part: LIGHT — INOPERATIVE (MID CABIN)

OAK - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS CONTROLLED BY POWER SUPPLY B5-27 WERE FOUND TO BE INOPERATIVE. REPAIRED CHAFED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DEFECTIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED LIGHT MODULE AND CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE AT ROWS 20-24. RECONNECTED MODULES AT ROW 24. LIGHT THEN OPERATED NORMALLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 8. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — LOOSE (CABIN)

PDX - DURING SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 6-7. RESECURED ELECTRICAL WIRING TO LAMP MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE MAINTENANCE CHECK, OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED NORMALLY. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR)

SEA - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. RESECURED LANYARD. (M)

Part: LIGHT — DAMAGED (CABIN)

YVR - DURING PREFLIGHT CHECK, FOUND AN EMERGENCY FLOOR TRACK LIGHT BROKEN AT ROW 6. REPLACED LIGHT ASSEMBLIES AT ROW 6. LGIHTS THEN OPERATED NORMALLY. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED 30K CHECK, FOUND STATION 570-577 LONGERON 18R WEB WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED 30K CHECK, THE UPPER SURFACE OF THE FLOOR WEB AT STATION 785, LONGERON 18R WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)

Part: LIGHT — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. RESEATED LIGHT ASSEMBLY CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

OAK - DURING LINE CHECK, OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED LIGHT BULBS AND ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, INTERIOR EMERGENCY OVERHEAD LIGHTS BETWEEN THE AFT LAVATORIES WERE DETERMINED TO BE INOPERATIVE. REPLACED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LAMP — INOPERATIVE (ROW 12)

SEA - FLT 650 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 12 WERE FOUND INOPERATIVE. REPLACED THE LAMP MODULE ASSY AND THE LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DAMAGED (CABIN)

SEA - PRIOR TO FLIGHT 604, THE EMERGENCY EXIT TRACK LIGHTS WERE REPORTED INOPERATIVE. INSPECTED AND FOUND A FAULTY BATTERY CONNECTION IN THE BATTERY PACK. REPAIRED CONNECTION, LIGHTS OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (AFT CABIN)

SAN - PRIOR TO FLIGHT 571 - THE EMERGENCY FLOOR TRACK LIGHTS AT ROWS 23-28 WERE FOUND TO BE INOPERATIVE. CONTRACT MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12-14 AND 21-29 WERE FOUND TO BE INOPERATIVE. REPLACED WIRING HARNESS FOR ROWS 12-14 AND REPLACED BATTERY PACK FOR ROWS 21-29, ALL LIGHTS OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12-14 AND 21-29 WERE FOUND TO BE INOPERATIVE. REPLACED WIRING HARNESS FOR ROWS 12-14 AND REPLACED BATTERY PACK FOR ROWS 21-29, ALL LIGHTS OPERATED NORMALLY. REF ASAA0080583.(M)

Part: CONTACTOR — DIRTY (BATTERY PACK)

ANC - DURING MAINTENANCE CHECK, THE MID TO AFT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. CLEANED CONTACTS ON BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - AFTER ARRIVAL OF FLIGHT 759, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT COVER DAMAGED AND SECTIONS OF THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR TRACK AT ROW 28 AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROW 21 TO 29 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: RELAY — INTERMITTENT (OVERWING) · airframe 27,592 hrs · 14,053 cycles

PHX - DUIRNG 30K CHECK, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. RELEASED PER MEL 33-20. SUBSEQUENTLY, REPLACED RELAY R2-271 IN ANC ON 4-1-00 AND LIGHTS OPERATED NORMALLY. (X)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN SEAT TRACK, LEFT INBOARD FS 1152 WAS FOUND CORRODED. REPAIRED PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN WEB AT FS 1032 LEFT, LONGERON 18 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE UPPER SURFACE OF THE CUSP WEB WAS FOUND CORRODED AT FS 1023-1098, STRINGER 18R. REMOVED CORROSION AND REPAIRED PER SRM 53-01. (M)

Part: POWER SUPPLY — DISCHARGED (LT OVERWING)

PHX - DURING 30K CHECK, THE LEFT AND RIGHT OVERWING EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED RELAY R2-271 AND EMERGENCY EXIT LIGHT POWER SUPPLY, LIGHTS OPERATED NORMALLY. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE SUBFLOOR FROM FS 160-200, RBL 50 - LBL 45 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-14-1, 53-01 AND 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30 CHECK, THE CUSP WEB AT FS 634, LONGERON 18R WAS FOUND CORRODED. REMOVED CORRODED AND REPAIRED PER SRM 51-30. (M)

Part: POWER SUPPLY — DISCHARGED (OVERWING EXITS)

PHX - DURING 30K CHECK, THE OVERWING EVACUATION LIGHTS WOULD NOT TEST. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, TOP OF LONGERON 30 WAS FOUND CORRODED AT FS 1083-1129. REMOVED CORROSION AND REPAIRED PER EA 5310-01806. (M)

Part: SKIN — GOUGED (FUSELAGE)

PHX - DURING 30K CHECK, THE SKIN AT FS 1174-1211, LONGERON 29L-29R WAS FOUND WITH OVERSIZED HOLES, LIGHT CORROSION AND GOUGES. REMOVED CORROSION AND REPAIRED PER AS EA 5330-01426 AND AMS EA 10-5330-0332. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, AFT CABIN, L2 DOOR ENTRY WAY, LEFT OUTBOARD SEAT TRACK WAS FOUND CORRODED AROUND NUTPLATE HOLES ON TOP AND BOTTOM SIDE AT FS 1155-1170, LBL 42. REMOVED CORROSION AND REPAIRED PER SRM 53-05, FIG 4. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT INTERCOSTAL AT FS 1211-1216, LONGERON 29L WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 51-30 AND 53-14-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 30 K CHECK, THE RIGHT AFT LAVATORY TOP SURFACES OF FRAME WERE FOUND TO HAVE EXFOLIATED CORROSION AROUND THE NUTPLATE HOLE, FS 1338, RBL 39. REMOVED CORROSION AND REPAIRED PER EA 5310-01805. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

PHX - DURING 30K CHECK, TEH LEFT AFT LAVATORY TOP SURFACE OF THE FLOORBEAM WAS FOUND WITH AN ELONGATED HOLE AND CORRODED AROUND THE NUTPLATE. REMOVED CORROSION AND REPAIRED PER EA 5310-01805. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE LONGERON AT FS 1022-1271, STRINGER 18R WAS FOUND CORRODED ON THE UPPER SURFACE OF THE FLOOR WEB. REMOVED CORROSION AND REPAIRED PER SRM 53-01. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TOP OF LONGERON 30 WAS FOUND CORRODED AT FS 1210-1297. REMOVED CORROSION AND REPAIRED PER SRM 53-14-3. (M)

Part: CLIP — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT MAIN FRAME TIE CLIP WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER AS EA 5330-01426 AND AMS EA 10-5330-0332. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, THE LEFT CUSP WEB AT FS 1300 WAS FOUND CRACKED. REPAIRED PER SRM 51-30. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT RIGHT TIEDOWN TRACK TO FLOOR PANEL TRANSITION Z-CHANNEL WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT DOOR BEAM AT FS 1173, LONGERON 29R WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 51-30. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND A DENT WAS FOUND IN THE FUSELAGE SKIN, 27 INCHES FORWARD OF THE LAVATORY ACCESS PANEL, BELOW STRINGER 18 AND AFT OF L1 DOOR. REPAIRED PER SRM 53-04, FIG 25 AND DWG J0600270. (M)

Part: CONNECTOR — UNSECURE (ROW 20)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 WERE FOUND INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMEGENCY LIGHTS FROM ROWS 19 TO 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER USPPLY AND OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT HALF OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE DIM. REPLACED TWO AFT BATTERIES IN EMERGENCY PACKS AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BULB — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THREE EMERGENCY FLOOR TRACK RED LIGHTS AT THE OVERWING EXITS WERE FOUND INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (ROW 21)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (ROW 13-18)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK RED LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUD INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID-CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (ROW 3)

SEA - PRIOR TO DEPARTURE OF FLIGHT 612, CREW REPORTED THE EMERGENCY FLOOR TRACK RED LIGHTS WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: SLIDE — FAILED (PAX DOOR)

OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRE IN FLOOR TRACK AT ROW 10 AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LAMP — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THREE RED EMERGENCY FLOOR TRACK LIGHTS AT ROW 21 WERE FOUND INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND DIM. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LAMP — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M)

Part: LIGHT — FAILED TEST (TAILCONE)

OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M)

Part: LIGHT — INOPERATIVE (L-1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LATCH — INOPERATIVE (R-2 DOOR)

ANC - FLT 202 - CREW REPORTED, R-2 DOOR LATCH INOPERATIVE. TIGHTENED DOOR LATCH AND OPERATED NORMALLY. (M)

Part: RETAINING PIN — SHEARED (L2 DOOR)

SEA - AFTER ARRIVAL OF FLT 367 - CREW REPORTED THE L2 DOOR HANDLE WAS TOO CLOSE TO THE DOOR TRIM MAKING IT DIFFICULT TO GRASP HANDLE FOR RAPID OPENING. REPLACED SHEARED HANDLE RETAINING PIN AND OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THREE RED EMERGENCY FLOOR TRACK LIGHTS AT ROW 21 WERE FOUND INOPERATIVE. RESET CONNECTOR AT FORWARD LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ONT - PRIOR TO DEPARTURE OF FLIGHT 531, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 21 TO 24 WERE INOPERATIVE. RECONNECTED WIRING AT ROW 24 AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED SECTION OF FLOOR TRACK LIGHTS AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SAN - PRIOR TO DEPARTURE OF FLIGHT 343, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED TRACK WIRING AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 620, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED TRACK WIRING AND OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 3 FORWARD. REPLACED DAMAGED LIGHT ASSEMBLY AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. SECURED LOOSE CONNECTOR AND OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 85, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOSE CONNECTOR AT ROW 3 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - FLT 204 - CREW REPORTED FIRST CLASS EMERGENCY EXIT FLOOR TRACK LIGHTS INOP IN FIRST CLASS CABIN. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - FLT 304 - FORWARD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE. REPLACED BATTERIES IN SECOND PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: SOCKET — LOOSE (CABIN)

ANC - PRIOR TO DEPARTURE OF FLT 84, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LIGHT SOCKET AT ROW 3 AND OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 85, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED ELECTRICAL CONNECTOR AND OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

BUR - PRIOR TO DEPARTURE OF FLT 535 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED ELECTRICAL CONNECTOR AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 32 AFT WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 32 AND OPERATED NORMALLY. (M)

Part: STRUT — REQ'D SERVICE (NLG)

ANC - AIR TURN BACK OF FLIGHT NR 82, CREW REPORTED, THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT LOW. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. (M)

Part: EEL WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD FOUR EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED WIRE HARNESS BETWEEN 4TH AND 5TH TRACK LIGHTS AND OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 15 AND 16 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: THROTTLE SWITCH — DEFECTIVE (COCKPIT)

SEA - FLT 574 - AIR TURN-BACK. CREW REPORTED ALL 3 GEAR RED LIGHTS ON AND GEAR WARNING HORN SOUNDED AFTER GEAR RETRACTED. CYCLED GEAR AND CONDITION REPEATED. REMOVED AND REPLACED THE LEFT THROTTLE SWITCH ASSEMBLY S319 AND OPERATED NORMALLY. (X)

Part: TRACK EEL — INOP (CABIN)

PDX - FIRST CLASS EMERGENCY TRACK LIGHTING INOP. MAINTENANCE FOUND TRACK COVER MISSING AND LIGHT ASSEMBLY UNPLUGGED. RECONNECTED PLUG AND REPLACED MISSING TRACK COVER. (Z)

Part: EEL TRACK COVER — MISSING (CABIN)

PDX - CHECK, FIRST CLASS EMERGENCY TRACK LIGHTING INOP. MAINTENANCE FOUND TRACK COVER MISSING AND LIGHT ASSEMBLY UNPLUGGED. RECONNECTED PLUG AND REPLACED MISSING TRACK COVER. REF 95ZZZW108.

Part: EEL TRACK COVER — MISSING (CABIN)

PDX - CHECK, FIRST CLASS EMERGENCY TRACK LIGHTING INOP. MAINTENANCE FOUND TRACK COVER MISSING AND LIGHT ASSEMBLY UNPLUGGED. RECONNECTED PLUG AND REPLACED MISSING TRACK COVER. REF ASAA9525.

Part: EEL POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (W)